发明授权
US09322293B2 Turbojet venting pipe, method for mounting one such pipe and turbojet provided with one such pipe 有权
涡轮喷气通风管,一个这种管道的安装方法和一个这样的管道的涡轮喷气发动机

Turbojet venting pipe, method for mounting one such pipe and turbojet provided with one such pipe
摘要:
A venting pipe used to guide a gas stream in a turbojet including at least one hollow rotary shaft inside which the pipe is mounted, the pipe extending generally along an axis. The pipe includes at least two pipe segments configured to be aligned longitudinally and assembled to one another while retaining a degree of freedom in relative translation thereof, at least one of the segments including a deformable mechanism configured to deform radially as the pipe segments are tightened against one another in the shaft of the turbojet, to bear on the shaft. The pipe structure facilitates mounting of the pipe.
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